Simulation of glancing shock wave and boundary layer interaction /

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Bibliographic Details
Author / Creator:Hung, Ching-Mao.
Imprint:Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. :] : [For sale by the National Technical Information Service], [1989]
Description:10 pages : illustrations.
Language:English
Series:NASA technical memorandum ; 102233
NASA technical memorandum ; 102233.
Subject:Shock waves -- Mathematical models.
Laminar boundary layer.
Boundary layer separation.
Computational fluid dynamics.
Computerized simulation.
Fins.
Shock waves.
Three dimensional flow.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6504668
Hidden Bibliographic Details
Other authors / contributors:Ames Research Center.
Notes:"September 1989."
"A-89241"--Technical rept. documentation p.
Includes bibliographical references (pages 6-7).
505-60
Available via Internet from the NASA Technical Report Server web site. Address as of 8/29/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002654%5F1990002654.pdf; current access available via PURL.
GPO item no.:0830-D (MF)
0830-D (online)
Govt.docs classification:NAS 1.15:102233
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